Leg restraint device for side-facing seated vehicle occupants

ABSTRACT

A leg restraint for side-seated vehicle occupants, and including a leg-restraining member adapted for being mounted in proximity to a side-facing vehicle seat and selectively moveable between a deployed, outwardly-extending leg-protecting position and a retracted, non-leg interfering position, and an actuator positioned operatively proximate the leg-restraining member and responsive to a signal output by a sensor for deploying the leg-restraining member upon the occurrence of an abrupt deceleration of the vehicle sensed by the sensor. The actuator includes a cushion, and is adapted for being positioned for deployment between the leg-restraining member and the legs of the seat occupant. The cushion is positioned on the actuator to cushion the legs against direct impact against the deployed leg-restraining member.

CROSS-REFERENCE TO RELATED PATENT APPLICATIONS

This application is a continuation of and claims priority to co-pendingU.S. patent application Ser. No. 14/060,143, filed Oct. 22, 2013, thefull contents of which are incorporated into this application byreference, which is a continuation-in-part of and claims priority toco-pending U.S. patent application Ser. No. 13/907,079, filed May 31,2013, the full contents of which are incorporated into this applicationby reference.

TECHNICAL FIELD AND BACKGROUND OF THE INVENTION

The present invention relates to a leg restraint device for side-seatedvehicle occupants. In particular, the invention relates to a legrestraint device for side-seated occupant of, for example, corporateaircraft of the type offering side-facing seats for passengers. Thedisclosed invention has application in any form of vehicletransportation where passenger or occupant seats maybe mounted in aside-facing orientation in relation to the direction of forward travelof the vehicle, such as an aircraft. The FAA has released PolicyPS-ANM-25-03-R1 requiring leg flail prevention for occupants seated inside-facing seats when the occupant's upper leg is restricted by contactwith the seat itself and/or with an interior component. In order toprovide adequate occupant protection, the lower legs must also berestricted in a similar manner to avoid upper leg femur bone torsion.Thus, there is a need for a device that will provide this lower legsupport during a dynamic event such as a crash.

Violent or abrupt deceleration can cause high g-force lateral loading ona side-facing passenger, causing lateral leg movement and leg rotationabout the knee and femur. This can cause dislocations, muscle and tendoninjuries and fractures due to the restraint exerted on the passengers'torso by seat belts and/or arm rests while the legs are unrestrained.However, belts or similar restraints on the legs are not advisable dueto the additional time needed to remove the restraints, as well as thepossibility that injuries to the passenger may make it difficult foreither the passenger or emergency personnel to remove such restraints.

Therefore, there is a need for a type of leg restraint that providesprotection to the legs of side-facing seat occupants in the event of acrash or other rapid deceleration, while not inhibiting rapid egressfrom the seat after the event.

The leg flail prevention device disclosed in this application deploysautomatically and is designed to be triggered by the same sensor andtrigger that is used to deploy inflatable shoulder harness air bags alsoinstalled on the side-facing seat. As such, for installations thatrestrict the side-facing occupant's upper legs in the forward direction,the automatic leg flail prevention device is utilized to introduce thehigher level of occupant protection. In the embodiment disclosed in theapplication, a linear restraint panel presents the main restriction tothe occupant's lower legs to prevent leg flail. This restraint panel isdeployed by the inflation force of an attached air bag. Once the air bagdeploys the restraint panel, the portion of the air bag attached to therestraint panel further inflates between the restraint panel and the legto cushion the impact of the occupant's legs with the restraint panel.

SUMMARY OF THE INVENTION

It is therefore an object of the present invention to provide a legrestraint that provides protection to the legs of side-facing seatoccupants in the event of a crash or other rapid deceleration.

It is another object of the invention to provide a leg restraint devicethat provides protection to the legs of side-facing seat occupants inthe event of a crash or other rapid deceleration, while not inhibitingrapid egress from the seat after the event.

It is another object of the invention to provide a leg restraint devicethat provides protection to the lower legs of side-facing seat occupantsin the event of a crash or other rapid deceleration, but that need notbe deployed during taxi, take-off and landing (“TTOL”).

It is another object of the invention to provide a leg restraint thatincludes an air bag as a means of deploying a linear restraint panelthat acts to restrict lateral movement of the lower legs of aside-seated occupant.

It is another object of the invention to provide a leg restraint thatincludes a deployable air bag as a means of cushioning and restrictinglateral movement of the lower legs of a side-facing seat occupant.

It is another object of the invention to provide a leg restraint thatincludes a deployable air bag utilized to deploy outwardly from the seata linear restraint panel that acts to restrict lateral movement of thelower leg, whereupon the air bag continues deploying and serves thefurther purpose of cushioning and restricting lateral movement of thelower legs of a side-facing seat occupant.

These and other objects and advantages of the invention are achieved byproviding a leg restraint for side-seated vehicle occupants, andincluding a leg-restraining member adapted for being mounted inproximity to a side-facing vehicle seat and selectively moveable betweena deployed, outwardly-extending leg-protecting position and a retracted,non-leg interfering position, and an actuator positioned operativelyproximate the leg-restraining member and responsive to a signal outputby a sensor for deploying the leg-restraining member upon the occurrenceof an abrupt deceleration of the vehicle sensed by the sensor. Theactuator includes a cushion, and is adapted for being positioned fordeployment between the leg-restraining member and the legs of the seatoccupant. The cushion is positioned on the actuator to cushion the legsagainst direct impact against the deployed leg-restraining member.

According to another embodiment of the invention, a biasing membercooperates with the leg-restraining member to move the leg-restrainingmember into the retracted position after impact of an occupant's legagainst the leg-restraining member.

According to another embodiment of the invention, a leg restraint forside-seated vehicle occupants is provided, and includes aleg-restraining member adapted for being mounted in proximity to aside-facing vehicle seat and selectively moveable between a deployed,outwardly-extending leg-protecting position and a retracted, non-leginterfering position. An actuator is positioned operatively proximatethe leg-restraining member and responsive to a signal output by a sensorfor deploying the leg-restraining member upon the occurrence of anabrupt deceleration of the vehicle sensed by the sensor. The actuatorincludes a cushion, and is adapted for being positioned for deploymentbetween the leg-restraining member and the legs of the seat occupant,the cushion being positioned on the actuator to cushion the legs againstdirect impact against the deployed leg-restraining member. The actuatorduring a first phase deploys the leg-restraining member and during asecond phase the actuator moves into a position between theleg-restraining member and the legs of the seat occupant wherein thecushion protects the legs against direct impact against the deployedleg-restraining member.

According to another embodiment of the invention, a leg restraint forside-seated vehicle occupants is provided, and includes aleg-restraining member adapted for being mounted in proximity to aside-facing vehicle seat and selectively moveable between a deployed,outwardly-extending leg-protecting position and a retracted, non-leginterfering position. An actuator is positioned operatively proximatethe leg-restraining member and responsive to a signal output by a sensorfor deploying the leg-restraining member upon the occurrence of anabrupt deceleration of the vehicle sensed by the sensor. The actuatorincludes a cushion, and is adapted for being positioned for deploymentbetween the leg-restraining member and the legs of the seat occupant,the cushion being positioned on the actuator to cushion the legs againstdirect impact against the deployed leg-restraining member. The actuatorduring a first phase deploys the leg-restraining member, during a secondphase deploys to a position between the leg-restraining member and thelegs of the seat occupant and during a third phase deploys to a positionbeyond an outermost extent of the deployed leg-restraining member tocushion the legs against direct impact against the deployedleg-restraining member.

According to another embodiment of the invention, a leg restraint forside-seated vehicle occupants is provided that includes aleg-restraining member adapted for being mounted in proximity to aside-facing vehicle seat and selectively moveable between a deployed,outwardly-extending leg-protecting position and a retracted, non-leginterfering position. An actuator is positioned operatively proximatethe leg-restraining member and responsive to a signal output by a sensorfor deploying the leg-restraining member upon the occurrence of anabrupt deceleration of the vehicle sensed by the sensor. The actuatorincludes a cushion, and is adapted for being positioned for deploymentbetween the leg-restraining member and the legs of the seat occupant,the cushion being positioned on the actuator to cushion the legs againstdirect impact against the deployed leg-restraining member. A retractoris provided for returning the leg-restraining member back into itsretracted position upon the leg-restraining member reaching its fullydeployed position, wherein the retractor comprises a spring having abias that is initially overpowered by the operation of the actuator asthe leg-restraining member is deployed, and is biased to return theleg-restraining member to its retracted position as the actuatorretracts.

According to another embodiment of the invention, the cushion is shapedsuch that its widest extent is at its distal end.

According to another embodiment of the invention, the leg-restrainingdevice includes a restraint panel having relatively upright side walls.

According to another embodiment of the invention, a sensor is providedfor detecting abrupt movement of the vehicle in the direction of forwardtravel of the vehicle incident to an abrupt deceleration and outputtinga responsive signal to a trigger responsive to the signal from thesensor for activating the air bag.

According to another embodiment of the invention, a leg restraint isprovided, and is adapted for being mounted on a side-facing aircraftseat for protecting the legs of the seat occupant, and includes arestraint panel mounted in proximity .to the side-facing aircraft seatand selectively moveable between a deployed, laterally-extendingleg-protecting position and a retracted, non-leg interfering position. Asensor is provided for detecting abrupt movement of the vehicle in thedirection of forward travel of the vehicle incident to an abruptdeceleration and outputting a responsive signal. An actuator is mountedon the restraint panel in a normally retracted configuration and in aposition wherein, upon actuation, propels the restraint panel into thedeployed position and then retracts. A trigger responsive to the signaloutput by the sensor is provided for deploying the actuator, and abiasing member includes a spring that is initially overpowered by theoperation of the actuator as the restraint panel is deployed, and isbiased to return the restraint panel to its retracted position as theactuator retracts.

According to another embodiment of the invention, the restraint panel ismounted in a housing adapted for being positioned under the seat bottomof the side-facing aircraft seat.

According to another embodiment of the invention, the restraint panelincludes a slide mounted in the housing for movement on at least onestationary guide shuttle mounted on an inner surface of the housing.

According to another embodiment of the invention, the actuator includesa cushion, and is adapted for being positioned for deployment betweenthe restraint panel and the legs of the seat occupant to cushion thelegs against direct impact against the deployed leg-restraining member.

According to another embodiment of the invention, the actuator isadapted to deploy during a first phase to deploy the restraint panel andto further deploy during a second phase to a position between therestraint panel and the legs of the seat occupant to cushion the legsagainst direct impact against the deployed restraint panel.

According to another embodiment of the invention, the actuator isadapted to deploy during a first phase to deploy the restraint panel andto further deploy during a second phase to position the cushion betweenthe restraint panel and the legs of the seat occupant and beyond theoutermost extent of the deployed restraint panel to cushion the legsagainst direct impact against the deployed restraint panel.

According to another embodiment of the invention, a spring is providedfor returning the leg-restraining member back into its retractedposition upon the leg-restraining member reaching its fully deployedposition.

According to another embodiment of the invention, the spring has a biasthat is initially overpowered by the operation of the actuator as theleg-restraining member is deployed, and is biased to return theleg-restraining member to its retracted position as the actuatorretracts.

According to another embodiment of the invention, the actuator has ashape that has its widest extent at its distal end and adapted toproject outwardly beyond the distal end of the restraint panel at itsfullest deployed extent.

According to another embodiment of the invention, the restraint panelincludes a recess extending along a length of the restraint panel, and aguide shuttle mounted on the housing and having wheels engaging opposingtop and bottom sides of the recess to guide the restraint panel betweenits retracted and deployed positions.

BRIEF DESCRIPTION OF THE DRAWING FIGURES

The present invention is best understood when the following detaileddescription of the invention is read with reference to the accompanyingdrawings, in which:

FIG. 1 is a perspective view of a side-seated aircraft seat, showing aleg restraint device according to a preferred embodiment of theinvention in its retracted position;

FIG. 2 is a side elevation of a side-seated aircraft seat, showing a legrestraint device according to a preferred embodiment of the invention inits retracted position;

FIG. 3 is a perspective view of a side-seated aircraft seat, showing aleg restraint device according to a preferred embodiment of theinvention in its deployed position;

FIG. 4 is a side elevation of a side-seated seat, showing a legrestraint device according to a preferred embodiment of the invention inits deployed position;

FIG. 5 is a partially-exploded view of one embodiment of the inventionshowing the air bag in its stowed, retracted position;

FIG. 6 is a partially-exploded view of one embodiment of the inventionshowing the air bag in its fully deployed position;

FIG. 7 is a vertical cross-section taken along line 7-7 of FIG. 5;

FIG. 8 is an exploded view of one embodiment of the invention from aside opposite FIGS. 5 and 6; and

FIG. 9 is a vertical cross-section taken along line 9-9 of FIG. 8.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT

Referring now specifically to the drawings, the environment of thedisclosure is an aircraft of the type having side-facing seats, such asseat 10, having a seat bottom 12, seat back 14 and an armrest/end bay16. Accordingly, a seat occupant sits with his or her back to theaircraft fuselage “A”, facing outward in a generally perpendiculardirection in relation to the longitudinal dimension of the aircraft andits direction of forward travel. For this reason, the occupant issubject to substantial lateral g-force loading along the longitudinalaxis of the aircraft in the event of an abrupt deceleration such asmight result during hard braking or a forward-directed crash event.While the upper torso and the thigh area of the legs are restrained tosome extent by the armrest 16 and the seat belt 18, the lower legs arefree to be projected laterally forward, rotating violently around anaxis defined by the knees, causing potential serious injury to both theknees and lower legs unless they are restrained in some mariner. Injuryto the legs is a particularly serious concern since such injuries couldprevent a passenger from being able to egress unaided from the aircraftin the event of an accident.

Thus, in accordance with the invention, a leg restraint device 20 isprovided. As shown in FIGS. 1 and 2, the leg restraint device 20 ismounted under the seat 10 forward of the occupant in relation to theaircraft's direction of forward travel. The leg restraint device 20includes two principal elements a housing 22 mounted under the seat 10,and a deployable restraint panel 24, which includes a cap plate 28 onthe distal end. During boarding, deplaning and normal flight, the legrestraint device 20 remains in a retracted condition, as shown in FIGS.1 and 2. In the event of an emergency that may result in an abruptdeceleration, the restraint panel 24 is automatically deployed, asexplained below.

The leg restraint device 20 as shown in the Figures is a “left-hand”oriented device shown mounted under a seat 10 and a left-hand side ofthe aircraft fuselage “A”, from the position of the seat occupant. Aright-hand device constructed in accordance with the invention would beutilized on seats facing inward from the right-hand side of the aircraftfuselage “A.” In general, the left and right-hand versions both requiremounting an air bag in a housing so that the air bag inflates againstthe leg of a seat occupant seated in a seat facing inward from the sideof the aircraft fuselage, and are mirror constructions of each other.

As shown in FIGS. 3 and 4, the restraint panel 24, when deployed,projects forwardly of the seat 10 into a position where the legs of theseat occupant are positioned behind the restraint panel 24 in relationto the aircraft's direction of forward travel. In the event of an actualabrupt deceleration of the aircraft, the occupant's legs are preventedfrom continued unrestrained forward motion by the restraint panel 24. Asdescribed in further detail below, the restraint panel 24 is deployed bythe inflation force imposed on the restraint panel 24 by an air bag 26that is stored in the housing 22. Upon the occurrence of an eventrequiring side restraint protection of the seat occupant, the air bag 26is triggered and during a first phase inflates and deploys the restraintpanel 24 by forcing it rapidly out of the end of the housing 22.

During a second phase of the deployment of the air bag 26, it continuesinflating and projects outwardly along the side of the deployedrestraint panel 24 nearest the seat occupant's foot and lower leg. Inthis configuration, shown in FIGS. 3 and 4, the air bag 26 provides anair cushion between the seat occupant's feet and lower legs thatprevents direct contact with the inner side of the restraint panel 24.Note that in its fully deployed configuration, the air bag 26 extendsbeyond the fully deployed position of the cap plate 28 of the restraintpanel 24 in order to fully protect the seat occupant's feet and lowerlegs.

The restraint panel 24 is caused to retract back in to the housing 22 bythe rapid deflation of the air bag 26, as is typical of air bagoperation. This retraction occurs very rapidly and thus clears the areaaround the seat 10 for rapid, unrestricted egress by both the seatoccupant and other aircraft occupants who may have to move past the seat10 in order to egress from the aircraft.

Referring now to FIGS. 4-9, the housing 22 of the restraint device 20 isformed from two stationary housing covers 30, 32. The restraint panel 24and the cap plate 28 slide in and out of the retracted and deployedpositions on a wheeled guide shuttle 34 mounted on the inner surface ofhousing cover 32. Note that the restraint panel 24 has a “corrugated”cross-section, FIGS. 7 and 9, which provides the necessary spacing forthe movable components. The guide shuttle 34 is captured in and ridesalong a central, longitudinally-extending recess 36 in the restraintpanel 24.

The restraint panel 24 is attached to a retractor that includes a springhousing 38 mounted on the cover 30. A vertical pin 40 mounts a coiledsteel spring 42 that is mounted on the restraint panel 24 and biasedtowards its retracted position. See FIG. 5. Activation of the air bag 26overcomes the bias of the spring 42 during inflation, allowing therestraint panel 24 to deploy, as shown in FIG. 6. As inflation ends anddeflation begins, the spring 42 causes the restraint panel 24 toimmediately retract so that, as described above, the restraint panel 24does not project into the aircraft aisle impeding egress from theaircraft.

The air bag 26 is mounted on and extends along the length of therestraint panel 24. As is shown in FIG. 5, the air bag 26, beforedeployment, resides in a deflated configuration against the restraintpanel 24. The air bag 26 includes a tubular neck 44 that is attached toan inflator 46 mounted on the cover 32. In the deflated configuration,the neck 44 is folded in an accordion manner between the inflator 46 andthe air bag 26. The term “air bag” is generally used to describe thisdevice even though gases other than “air” cause the bag to inflate. Theinflator 46 may be a cold gas inflator, a hybrid inflator, or apyrotechnic inflator depending on the design factors of the device.Speed, deployment time, gas temperature, etc. can all dictate the typeof inflator 46 utilized to achieve the desired operation and may be thesubject of varying legal and technical requirements.

The inflator 46 may be triggered by a trigger/sensor 48 that is alsoused to activate the seat belt 18, see FIG. 6, or by a trigger/sensorthat functions only to inflate the air bag 26. As shown in FIGS. 5 and6, the trigger/sensor 48 communicates with the inflator 46 through ashielded conduit 50. As shown in FIG. 6, inflation of the air bag 26causes the neck 44 to first inflate as gas passes from the inflator 46to the air bag 26. This inflation causes the neck 44 to unfold andstraighten, driving the air bag 28 and the restraint panel 24 on whichit is mounted rapidly forward out of the housing 22 and into the aisleof the aircraft, as shown in FIGS. 3 and 4. Typically, the air bag 26 isfully inflated within approximately 60-80 milliseconds, and vents in theair bag 26 allow the gas to escape, very rapidly deflating the air bag26. The spring 42 rapidly returns the restraint panel 24 and air bag 26to the position shown in FIG. 5, as described above.

A leg restraint device for side-seated vehicle occupants according tothe invention has been described with reference to specific embodimentsand examples. Various details of the invention may be changed withoutdeparting from the scope of the invention. Furthermore, the foregoingdescription of the preferred embodiments of the invention and best modefor practicing the invention are provided for the purpose ofillustration only and not for the purpose of limitation, the inventionbeing defined by the claims.

What is claimed is:
 1. A leg restraint for side-seated vehicleoccupants, and comprising: (a) a leg-restraining member adapted forbeing mounted in proximity to a side-facing vehicle seat and selectivelymoveable between a deployed, outwardly-extending leg-protecting positionand a retracted, non-leg interfering position; (b) an actuatorpositioned operatively proximate the leg-restraining member andresponsive to a signal output by a sensor for deploying theleg-restraining member upon the occurrence of an abrupt deceleration ofthe vehicle sensed by the sensor; and (c) wherein the actuator includesa cushion, and is adapted for being positioned for deployment betweenthe leg-restraining member and the legs of the seat occupant, thecushion being positioned on the actuator to cushion the legs againstdirect impact against the deployed leg-restraining member.
 2. A legrestraint according to claim 1, and including a biasing membercooperating with the leg-restraining member to move the leg-restrainingmember into the retracted position after impact of an occupant's legagainst the leg-restraining member.
 3. A leg restraint for side-seatedvehicle occupants, and comprising: (a) a leg-restraining member adaptedfor being mounted in proximity to a side-facing vehicle seat andselectively moveable between a deployed, outwardly-extendingleg-protecting position and a retracted, non-leg interfering position;(b) an actuator positioned operatively proximate the leg-restrainingmember and responsive to a signal output by a sensor for deploying theleg-restraining member upon the occurrence of an abrupt deceleration ofthe vehicle sensed by the sensor; (c) wherein the actuator includes acushion, and is adapted for being positioned for deployment between theleg-restraining member and the legs of the seat occupant, the cushionbeing positioned on the actuator to cushion the legs against directimpact against the deployed leg-restraining member; and (d) furtherwherein the actuator during a first phase deploys the leg-restrainingmember and during a second phase the actuator moves into a positionbetween the leg-restraining member and the legs of the seat occupantwherein the cushion protects the legs against direct impact against thedeployed leg-restraining member,
 4. A leg restraint for side-seatedvehicle occupants, and comprising: (a) a leg-restraining member adaptedfor being mounted in proximity to a side-facing vehicle seat andselectively moveable between a deployed, outwardly-extendingleg-protecting position and a retracted, non-leg interfering position;(b) an actuator positioned operatively proximate the leg-restrainingmember and responsive to a signal output by a sensor for deploying theleg-restraining member upon the occurrence of an abrupt deceleration ofthe vehicle sensed by the sensor; (c) wherein the actuator includes acushion, and is adapted for being positioned for deployment between theleg-restraining member and the legs of the seat occupant, the cushionbeing positioned on the actuator to cushion the legs against directimpact against the deployed leg-restraining member; and (d) furtherwherein the actuator during a first phase deploys the leg-restrainingmember, during a second phase deploys to a position between theleg-restraining member and the legs of the seat occupant and during athird phase deploys to a position beyond an outermost extent of thedeployed leg-restraining member to cushion the legs against directimpact against the deployed leg-restraining member.
 5. A leg restraintfor side-seated vehicle occupants, and comprising:, (a) aleg-restraining member adapted for being mounted in proximity to aside-facing vehicle seat and selectively moveable between a deployed,outwardly-extending leg-protecting position and a retracted, non-leginterfering position; (b) an actuator positioned operatively proximatethe leg-restraining member and responsive to a signal output by a sensorfor deploying the leg-restraining member upon the occurrence of anabrupt deceleration of the vehicle sensed by the sensor; (c) wherein theactuator includes a cushion, and is adapted for being positioned fordeployment between the leg-restraining member and the legs of the seatoccupant, the cushion being positioned on the actuator to cushion thelegs against direct impact against the deployed leg-restraining member;and (d) a retractor for returning the leg-restraining member back intoits retracted position upon the leg-restraining member reaching itsfully deployed position, wherein the retractor comprises a spring havinga bias that is initially overpowered by the operation of the actuator asthe leg-restraining member is deployed, and is biased to return theleg-restraining member to its retracted position as the actuatorretracts.
 6. A leg restraint according to claim 5, wherein the cushionis shaped such that its widest extent is at its distal end.
 7. A legrestraint according to claim 1, wherein the leg-restraining devicecomprises a restraint panel having relatively upright side walls.
 8. Aleg restraint according to claim 1, and including a sensor for detectingabrupt movement of the vehicle in the direction of forward travel of thevehicle incident to an abrupt deceleration and outputting a responsivesignal to a trigger responsive to the signal from the sensor foractivating the air bag.
 9. A leg restraint adapted for being mounted ona side-facing aircraft seat for protecting the legs of the seatoccupant, and comprising; (a) a restraint panel mounted in proximity tothe side-facing aircraft seat and selectively moveable between adeployed, laterally-extending leg-protecting position and a retracted,non-leg interfering position; (b) a sensor for detecting abrupt movementof the vehicle in the direction of forward travel of the vehicleincident to an abrupt deceleration and outputting a responsive signal;(c) an actuator mounted on the restraint panel in a normally retractedconfiguration and in a position wherein, upon actuation, propels therestraint panel into the deployed position and then retracts; (d) atrigger responsive to the signal output by the sensor for deploying theactuator; and (e) a biasing member comprising a spring that is initiallyoverpowered by the operation of the actuator as the restraint panel isdeployed, and is biased to return the restraint panel to its retractedposition as the actuator retracts.
 10. A leg restraint according toclaim 9, wherein the restraint panel is mounted in a housing adapted forbeing positioned under the seat bottom of the side-facing aircraft seat.11. A leg restraint according to claim 10, wherein the restraint panelcomprises a slide mounted in the housing for movement on at least onestationary guide shuttle mounted on an inner surface of the housing. 12.A leg restraint according to claim 11, wherein the actuator includes acushion, and is adapted for being positioned for deployment between therestraint panel and the legs of the seat occupant to cushion the legsagainst direct impact against the deployed leg-restraining member.
 13. Aleg restraint according to claim 12, wherein the actuator is adapted todeploy during a first phase to deploy the restraint panel and to furtherdeploy during a second phase to a position between the restraint paneland the legs of the seat occupant to cushion the legs against directimpact against the deployed restraint panel.
 14. A leg restraintaccording to claim 13, wherein the actuator is adapted to deploy duringa first phase to deploy the restraint panel and to further deploy duringa second phase to position the cushion between the restraint panel andthe legs of the seat occupant and beyond the outermost extent of thedeployed restraint panel to cushion the legs against direct impactagainst the deployed restraint panel.
 15. A leg restraint according toclaim 9, and including a spring for returning the leg-restraining memberback into its retracted position upon the leg-restraining memberreaching its fully deployed position.
 16. A leg restraint according toclaim 15, wherein the spring has a bias that is initially overpowered bythe operation of the actuator as the leg-restraining member is deployed,and is biased to return the leg-restraining member to its retractedposition as the actuator retracts.
 17. A leg restraint according toclaim 12, wherein the actuator has a shape that has its widest extent atits distal end and adapted to project outwardly beyond the distal end ofthe restraint panel at its fullest deployed extent.
 18. A leg restraintaccording to claim 12, wherein the restraint panel includes a recessextending along a length of the restraint panel, and a guide shuttlemounted on the housing and having wheels engaging opposing top andbottom sides of the recess to guide the restraint panel between itsretracted and deployed positions.